IRIDIUM 133
Satellite information IRIDIUM 133 - Iridium Next SV133
| Spacetrack Directory Name | IRIDIUM 133 |
| Alternative name | Iridium Next SV133 |
| Group | IRIDIUM |
| Follow IRIDIUM 133 | IRIDIUM 133 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 133 | Pass predictions IRIDIUM 133 |
| Orbit launches |
2017-10-09 (9 years ago)
|
| Days in orbit | 3288 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 133 | 789.86 km |
Additional information IRIDIUM 133
IRIDIUM 133, also known as Iridium Next SV133, is a communication and traffic monitoring satellite owned by IRIDS and manufactured by OATKGA. Launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has a design life of 10 years with plans for an extended operation up to 15 years. It measures 3.1 meters in length and 1.5 meters in diameter, with a span of 9.4 meters. The dry mass is recorded at 700 kilograms, while the launch mass was 860 kilograms. Equipped with L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver, it utilizes two deployable solar arrays and batteries for power supply. Its shape is described as a half hex prism with two panels.
satellite IRIDIUM 133 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 133 hundred 789.86 km. Average velocity IRIDIUM 133 is 26856.99 km/h. Inclination IRIDIUM 133 satellite 86.4°.TLE
Average velocity IRIDIUM 133
Average inclination IRIDIUM 133
Mean right ascension of the ascending node (RAAN) IRIDIUM 133
Mean argument of perigee IRIDIUM 133
Mean semi-major axis of the orbit IRIDIUM 133
Mean orbital eccentricity IRIDIUM 133
ISS
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